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master's thesis
Analiza ravnotežnog leta helikoptera
Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. urn:nbn:hr:235:272044
Jurišić, Antonio
University of Zagreb
Faculty of Mechanical Engineering and Naval Architecture

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Jurišić, A. (2019). Analiza ravnotežnog leta helikoptera (Master's thesis). Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture. Retrieved from https://urn.nsk.hr/urn:nbn:hr:235:272044

Jurišić, Antonio. "Analiza ravnotežnog leta helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. https://urn.nsk.hr/urn:nbn:hr:235:272044

Jurišić, Antonio. "Analiza ravnotežnog leta helikoptera." Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, 2019. https://urn.nsk.hr/urn:nbn:hr:235:272044

Jurišić, A. (2019). 'Analiza ravnotežnog leta helikoptera', Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, accessed 20 April 2024, https://urn.nsk.hr/urn:nbn:hr:235:272044

Jurišić A. Analiza ravnotežnog leta helikoptera [Master's thesis]. Zagreb: University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture; 2019 [cited 2024 April 20] Available at: https://urn.nsk.hr/urn:nbn:hr:235:272044

A. Jurišić, "Analiza ravnotežnog leta helikoptera", Master's thesis, University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Zagreb, 2019. Available at: https://urn.nsk.hr/urn:nbn:hr:235:272044

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Metadata
TitleAnaliza ravnotežnog leta helikoptera
Title (english)Helicopter trim analysis
AuthorAntonio Jurišić
MentorMilan Vrdoljak (mentor)
GranterUniversity of Zagreb
Faculty of Mechanical Engineering and Naval Architecture
Zagreb
Defense date and country2019-07-10, Croatia
Scientific / art field,
discipline and subdiscipline		TECHNICAL SCIENCES
Aviation, Rocket and Space Technology
Abstract
U ovom diplomskom radu provedena je analiza ravnotežnog leta helikoptera konvencionalne konfiguracije s glavnim i repnim rotorom. Opisane su geometrijske, inercijalne i aerodinamičke karakteristike helikoptera pri čemu sile i momenti koji djeluju na helikopter, osim glavnog i repnog rotora, dolaze i od trupa, te horizontalnog i vertikalnog stabilizatora. Opisan je iterativni postupak izračuna potrebnih varijabli te je napravljen programski model ravnotežnog leta. Također, provedena je analiza parametara algoritma te su dobiveni rezultati, za tri različita helikoptera, uspoređeni sa drugim dostupnim modelima i sa podacima dobivenim tijekom leta.
Abstract (english)
In this master’s thesis trim analysis of a helicopter with a conventional configuration was carried out. The geometric, inertial and aerodynamic characteristics of the helicopter are described where forces and moments that act on the helicopter are caused by the main rotor, fuselage, empennage and tail rotor. An analytical description of the iterative procedure is also explained and a numerical model of flight trim was constructed. The parameter analysis was carried out and the results of the three different helicopters were compared with other available models and with data obtained during the flight.
Keywords
Keywords (english)
Languagecroatian
URN:NBNurn:nbn:hr:235:272044
Study programmeTitle: Aeronautical Studies
Study programme type: university
Study level: graduate
Academic / professional title: magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva (magistar/magistra inženjer/inženjerka zrakoplovnog inženjerstva)
Type of resourceText
File originBorn digital
Access conditionsOpen access
Terms of useLicence In copyright icon
RepositoryRepository of Faculty of Mechanical Engineering and Naval Architecture University of Zagreb
Created on2019-07-04 08:53:56

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